US3778261A - Manufacturing composite articles - Google Patents
Manufacturing composite articles Download PDFInfo
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- US3778261A US3778261A US00139837A US3778261DA US3778261A US 3778261 A US3778261 A US 3778261A US 00139837 A US00139837 A US 00139837A US 3778261D A US3778261D A US 3778261DA US 3778261 A US3778261 A US 3778261A
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- United States
- Prior art keywords
- matrix
- carbide
- carbonaceous material
- bonding
- metal
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C47/00—Making alloys containing metallic or non-metallic fibres or filaments
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/10—Alloys containing non-metals
- C22C1/1036—Alloys containing non-metals starting from a melt
Definitions
- a method of manufacturing a composite article comprises forming a metal matrix which includes a suitable carbide forming constituent contacting the matrix with a carbonaceous material to be incorporated in the matrix, and heating the matrix to a predetermined temperature below the melting point of the matrix for a sufficient length of time to induce the carbide forming constituent to diffuse through the matrix to the interface between the carbonaceous material and the matrix and react with the carbonaceous material to form a bonding carbide layer between the matrix and the carbonaceous material.
- Thisqinvention relates to methods of manufacturing composite articles comprising a metallic matrix to which is bonded carbonaceous material, and articles so produced.
- the invention is particularly, although not exclusively concerned with composite articles which incorporate, ,or are coated or impregnated with, carbonaceous materials such as for example carbon fibres, diamond abrasives or refractory metal carbides.
- An object of thepresent invention is to provide a solid state method of bondingcarbonaceous material in a matrix material.
- solidstate it is meant that the method of the present invention is carried out at temperatures below the melting'point of the matrix material, i.e., whilst the matrix is a solid and is thus distinguished from prior art processes for bonding diamonds in metal matrices whichrely on the melting ability of various materials and which are carried out at temperatures at which the matrix material is molten.
- the present invention is also distinguished over the prior art process which require the melting andfusing of a bronze material which is applied to the diamonds prior to contacting them with the matrix in which they are to be held.
- a method of manufacturing a composite article comprises forming a metal matrix which includes a suitable carbide forming constituent as herein defined, contacting the matrix with a carbonaceous material to be incorporated in the matrix, and heating the matrix to a predetermined temperature below the melting point of the matrix for a sufficient length of time to induce the carbide forming constituent to diffuse through the matrix to the interface between the carbonaceous material and the matrix and react with the carbonaceous material to form a bonding carbide layer between the matrix and the carbonaceous material.
- a method of manufacturing a composite article comprises forming a metal matrix from a metal powder mixturewhich includes a suitable carbide forming constituent as herein defined, forming the mixture into a green artefact, curing the green artefact to produce a cured artefact, contacting the cured artefact with a carbonaceous material and heating the cured artefact to a predetermined temperature below the melting point of the matrix for a sufficient length of time to induce the carbide forming constituent of the matrix to diffuse through the matrix to the interface between the carbonaceous material and the matrix and react with the carbonaceous material to form a bonding carbide layer between the matrix and the carbonaceous material.
- a method of manufacturing a composite article comprises forming a matrix from a powdered mixture which includes carbonaceous material and a sinterable carbide forming constituent, as herein defined forming the mixture into a green artefact, curing the green artefact, and heating to a predetermined temperature below the melting point of the cured artefact for a sufficient length of time to induce the carbide forming constituent of the matrix to diffuse through the matrix to the interface between the carbonaceous material and the matrix and react with the carbonaceous material to form a bonding carbide layer between the matrix and the carbonaceous material.
- the carbonaceous material may be an abrasive material such as for example diamond particles or refractory metal carbides or may be in the form of carbon fibres.
- the matrix may be formed from a copper based alloy, an aluminium based alloy, or a tin based alloy, and the suitable carbide forming constituents of the alloy may be, for example, one of the following metals: titanium, vanadium, chromium hafnium, manganese or iron.
- suitable carbide forming constituent it is meant one or more elements and/or an alloy of such elements which whist being compatible with the matrix material will react with the carbonaceous material at temperatures below the melting point of the matrix to form a carbide which is stable in the environment in which the final product is to be used.
- the carbide layer formed between the diamond and the matrix should not be soluble in water; in other words, the carbide bonding layer should not disintegrate during use of the product.
- Al C Ca C and Scandium carbides have been found to be unsuitable for bonding diamonds to metal matrices when used with a water based coolant as they are soluble in water.
- suitable carbide formers shall be taken to exclude carbide formers which will not react with the carbonaceous material to be incorporated in the matrix at temperatures below the melting point of the matrix and which will not diffuse through the matrix to the interface between the matrix and the carbonaceous material to form a bonding carbide layer.
- a matrix was constructed from a copper based alloy which contained 1.0 percent by weight of chromium.
- a surface of the matrix so formed was contacted with diamond particles of about 7-15 microns particle size, the matrix was heated to 900 to l,00OC for 16 hours in a vacuum at a pressure of 10" to 10" Torr and the diamonds were pressed into the matrix.
- Migration of the chromium content of the alloy to the interface between the matrix and the diamond particles formed an adherent bonding layer of carbide of a few microns thick.
- the present invention relies on the migration of a sinterable carbide former to form a carbide layer to bond the diamonds to the matrix, then if the size or number of diamond particles is altered it may be necessary to alter the amount of carbide former in the matrix. For example as the extent of the total surface area of diamond particles will increase by increasing the number or size of the diamonds so the amount of suitable carbide forming constituent may need to be increased to provide sufficient carbide former to migrate to the interface between the diamond and the matrix. A decrease in the size or number of diamond particles may necessitate a decrease in the amount of carbide formers in the matrix. Similarly by varying the rate of diffusion of the carbide former through the matrix the time for which the matrix is heated to permit the carbide to diffuse through the matrix a similar adjustment may be possible to take into account different.
- the times at which the matrix is heated to induce diffusion of the carbide former through the matrix are important and are determined by such parameters as the interfacial area, the concentration of the carbide former in the matrix and the temperature of heat treatment. It is believed that the relationship between these parameters may be expressed by a modified Lifshitz- Wagner equation namely:
- C is the concentration of carbide former in the matrix I is the time T is the temperature B is a constant It is our belief that the maximum useful concentration of suitable carbide forming element in the matrix will be approximately equal to its equilibrium solid solubility in the matrix metal.
- the carbonaceous material to be incorporated into the matrix is a refractory metal carbide, for example titanium carbide, or tungsten carbide or the like
- the carbide forming constituent of the matrix should be compatible with the matrix material and preferably be more reactive with the refractory metal carbide, than with the alloy forming the matrix. If such an alloy is heated to a temperature below its melting point for a sufficient length of time, migration of the carbide forming constituent in the matrix to the interface between the matrix and the refractory metal carbide occurs and a bonding carbide layer will be formed between the matrix and the refractory metal carbide.
- matrix may be made from metals which are non-reactive with carbonaceous materials, i.e., copper, lead and tin, and also metals such as aluminium which will react with carbonaceous material, but not strongly at temperatures below the melting point of the alloy, these metals are alloyed with one or more elements and are compatible with the matrix which will react readily with the carbonaceous material to effect bonding of the carbonaceous material to the matrix by the method of the present invention.
- carbide forming metals other than titanium, vanadium and hafnium which also appear in the fourth period of the period table of elements are suitable carbide formers, e.g., scandium calcium, manganese and iron.
- scandium carbide and Ca C are soluble in water and are not suitable for example, in bonding diamonds to grinding wheels which are to be used with water based coolants or in moist atmospheres.
- a further material to which we have bonded diamond particles by a solid state process is stainless steel (i.e., an iron based alloy containing nickel and chromium).
- the present invention may be used with advantage for incorporating carbon fibres in a metal matrix by dis,- tributing the carbon fibre throughout a powdered mixture of the matrix material either as a continuous tow or a chopped fibre and sintering the powdered mixture to produce a cured artefact containing the disperesed carbon fibres.
- the present invention greatly improves the bonding of the carbon fibres to the matrix material.
- a suitable carbide forming constituent that will react favourably with the carbon fibres to form an adherent bonding carbide layer a strong bonding carbide layer may be formed at the interface of the sintered matrix and the carbon fibre.
- the invention is not limited to the foregoing examples and if desired the carbide forming constituents may be implanted in the metal matrix by an ion implantation process or by a sputtering process.
- a solid state method of bonding a solid carbonaceous material selected from the group consisting of diamond, carbon fiber, and refractory metal carbides to a solid metal body which is principally of a metal which will not readily react with the carbonaceous material to form a carbide while the body is in the solid state comprising the steps of: incorporating in the body a metal carbide-forming constituent, said metal carbide forming constituent being dispersed within said body in a finely divided state; contacting the body with the carbonaceous material; heating the body to a temperature at which the body remains wholly solid and maintaining the body at the said temperature for a time sufficient to allow the metal carbide-forming constituent to diffuse through the body to the interface between the carbonaceous material and the body and to react in the solid state with the carbonaceous material to form a bonding carbide layer between the body and the carbonaceous material; the said metal carbide-forming constituent being one which will diffuse through the body and which will react in the solid state with the carbonaceous material to form a carbide, and the body being one
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Ceramic Products (AREA)
- Polishing Bodies And Polishing Tools (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
Abstract
A method of manufacturing a composite article comprises forming a metal matrix which includes a suitable carbide forming constituent contacting the matrix with a carbonaceous material to be incorporated in the matrix, and heating the matrix to a predetermined temperature below the melting point of the matrix for a sufficient length of time to induce the carbide forming constituent to diffuse through the matrix to the interface between the carbonaceous material and the matrix and react with the carbonaceous material to form a bonding carbide layer between the matrix and the carbonaceous material.
Description
United States Patent 91 Nicholas et a1.
[ MANUFACTURING COMPOSITE ARTICLES [75] Inventors: Michael George Nicholas, Wantage;
lain MacPahil, Reading, both of England [73] Assignee: United Kingdom Atomic Energy Authority, London, England [22], Filed: May 3, 1971 121] Appl. No.: 139,837
[30] Foreign Application Priority Data 1 Dec. 11, 1973 2,068,848 1/1937 De Bats 75/204 2,133,495 10/1938 Willey v t 75/204 2,134,305 10/1938 Kieffer 75/204 3,377,696 4/1968 Farrow 29/4729 Primary ExaminerCarl D. Quarforth Assistant ExaminerB. Hunt Attorney-Larson, Taylor & Hinds [57] ABSTRACT A method of manufacturing a composite article comprises forming a metal matrix which includes a suitable carbide forming constituent contacting the matrix with a carbonaceous material to be incorporated in the matrix, and heating the matrix to a predetermined temperature below the melting point of the matrix for a sufficient length of time to induce the carbide forming constituent to diffuse through the matrix to the interface between the carbonaceous material and the matrix and react with the carbonaceous material to form a bonding carbide layer between the matrix and the carbonaceous material.
8 Claims, No Drawings MANUFACTURING COMPOSITE ARTICLES Thisqinvention relates to methods of manufacturing composite articles comprising a metallic matrix to which is bonded carbonaceous material, and articles so produced. The invention is particularly, although not exclusively concerned with composite articles which incorporate, ,or are coated or impregnated with, carbonaceous materials such as for example carbon fibres, diamond abrasives or refractory metal carbides.
An object of thepresent invention is to provide a solid state method of bondingcarbonaceous material in a matrix material.
By. solidstate it is meant that the method of the present invention is carried out at temperatures below the melting'point of the matrix material, i.e., whilst the matrix is a solid and is thus distinguished from prior art processes for bonding diamonds in metal matrices whichrely on the melting ability of various materials and which are carried out at temperatures at which the matrix material is molten. The present invention is also distinguished over the prior art process which require the melting andfusing of a bronze material which is applied to the diamonds prior to contacting them with the matrix in which they are to be held.
According to the present invention a method of manufacturing a composite article comprises forming a metal matrix which includes a suitable carbide forming constituent as herein defined, contacting the matrix with a carbonaceous material to be incorporated in the matrix, and heating the matrix to a predetermined temperature below the melting point of the matrix for a sufficient length of time to induce the carbide forming constituent to diffuse through the matrix to the interface between the carbonaceous material and the matrix and react with the carbonaceous material to form a bonding carbide layer between the matrix and the carbonaceous material.
According to an aspect of the present invention a method of manufacturing a composite article comprises forming a metal matrix from a metal powder mixturewhich includes a suitable carbide forming constituent as herein defined, forming the mixture into a green artefact, curing the green artefact to produce a cured artefact, contacting the cured artefact with a carbonaceous material and heating the cured artefact to a predetermined temperature below the melting point of the matrix for a sufficient length of time to induce the carbide forming constituent of the matrix to diffuse through the matrix to the interface between the carbonaceous material and the matrix and react with the carbonaceous material to form a bonding carbide layer between the matrix and the carbonaceous material.
According to a further aspect of the present invention a method of manufacturing a composite article comprises forming a matrix from a powdered mixture which includes carbonaceous material and a sinterable carbide forming constituent, as herein defined forming the mixture into a green artefact, curing the green artefact, and heating to a predetermined temperature below the melting point of the cured artefact for a sufficient length of time to induce the carbide forming constituent of the matrix to diffuse through the matrix to the interface between the carbonaceous material and the matrix and react with the carbonaceous material to form a bonding carbide layer between the matrix and the carbonaceous material.
The carbonaceous material may be an abrasive material such as for example diamond particles or refractory metal carbides or may be in the form of carbon fibres.
Preferably the matrix may be formed from a copper based alloy, an aluminium based alloy, or a tin based alloy, and the suitable carbide forming constituents of the alloy may be, for example, one of the following metals: titanium, vanadium, chromium hafnium, manganese or iron.
By suitable carbide forming constituent" it is meant one or more elements and/or an alloy of such elements which whist being compatible with the matrix material will react with the carbonaceous material at temperatures below the melting point of the matrix to form a carbide which is stable in the environment in which the final product is to be used. For example, if the final product is a diamond grinding wheel which will be used with a water based coolant then the carbide layer formed between the diamond and the matrix should not be soluble in water; in other words, the carbide bonding layer should not disintegrate during use of the product. In this respect Al C Ca C and Scandium carbides have been found to be unsuitable for bonding diamonds to metal matrices when used with a water based coolant as they are soluble in water.
The term suitable carbide formers shall be taken to exclude carbide formers which will not react with the carbonaceous material to be incorporated in the matrix at temperatures below the melting point of the matrix and which will not diffuse through the matrix to the interface between the matrix and the carbonaceous material to form a bonding carbide layer.
According to yet a further aspect of the present invention there is provided an article manufactured in accordance with and one of the methods of manufacture of the present invention.
To enable the invention to be more readily understood the invention will now be described with reference to the following experiments.
In the first experiment a matrix was constructed from a copper based alloy which contained 1.0 percent by weight of chromium. A surface of the matrix so formed was contacted with diamond particles of about 7-15 microns particle size, the matrix was heated to 900 to l,00OC for 16 hours in a vacuum at a pressure of 10" to 10" Torr and the diamonds were pressed into the matrix. Migration of the chromium content of the alloy to the interface between the matrix and the diamond particles formed an adherent bonding layer of carbide of a few microns thick.
To establish the rate of growth of the carbide bonding layer between the matrix and a carbonaceous material, various heat treatment were carried out on a number of different specimens of selected alloys. For example a number of matrices were formed from copper based alloys containing 1 percent by weight of Cr. Each matrix was contacted with vitreous carbon instead of diamond and heated to 950C. This temperature was maintained for different lengths of time for different specimens. The specimens were sectioned and the thickness of the carbide layer between the vitreous carbon and the matrix measured. The following table (Table 1) shows some of the results obtained using a matrix of a non-ferrous copper alloy containing 1% Cr.
TABLE 1 Time in days at 950C From the above experiments concerning the bonding of copper based alloys to vitreous carbon it is reasonable to expect that similar results may be obtained when using diamonds or carbon fibres instead of vitreous carbon providing the matrix is heated to a temperature below the melting point of the matrix for sufficient length of time to allow the carbide forming element in the matrix to diffuse through the matrix and react with the carbonaceous material.
As the present invention relies on the migration of a sinterable carbide former to form a carbide layer to bond the diamonds to the matrix, then if the size or number of diamond particles is altered it may be necessary to alter the amount of carbide former in the matrix. For example as the extent of the total surface area of diamond particles will increase by increasing the number or size of the diamonds so the amount of suitable carbide forming constituent may need to be increased to provide sufficient carbide former to migrate to the interface between the diamond and the matrix. A decrease in the size or number of diamond particles may necessitate a decrease in the amount of carbide formers in the matrix. Similarly by varying the rate of diffusion of the carbide former through the matrix the time for which the matrix is heated to permit the carbide to diffuse through the matrix a similar adjustment may be possible to take into account different.
sizes or numbers of diamonds.
The times at which the matrix is heated to induce diffusion of the carbide former through the matrix are important and are determined by such parameters as the interfacial area, the concentration of the carbide former in the matrix and the temperature of heat treatment. It is believed that the relationship between these parameters may be expressed by a modified Lifshitz- Wagner equation namely:
A C (t/T) e where A is a constant related to the critical thickness of carbide bonding layer,
C is the concentration of carbide former in the matrix I is the time T is the temperature B is a constant It is our belief that the maximum useful concentration of suitable carbide forming element in the matrix will be approximately equal to its equilibrium solid solubility in the matrix metal.
When bonding diamonds into various matrices it is preferable to carry out the heat treatments in a neutral environment for example in argon (at a pressure of about 10 torr) or C or CO Oxidising atmospheres will degrade the diamond, and carburising atmospheres will compete with the diamond for the carbide forming constituent. Furthermore the best results are achieved at temperatures at which graphitisation of the diamond is minimal.
Furthermore if the carbonaceous material to be incorporated into the matrix is a refractory metal carbide, for example titanium carbide, or tungsten carbide or the like, then the carbide forming constituent of the matrix should be compatible with the matrix material and preferably be more reactive with the refractory metal carbide, than with the alloy forming the matrix. If such an alloy is heated to a temperature below its melting point for a sufficient length of time, migration of the carbide forming constituent in the matrix to the interface between the matrix and the refractory metal carbide occurs and a bonding carbide layer will be formed between the matrix and the refractory metal carbide.
It is to be understood that matrix may be made from metals which are non-reactive with carbonaceous materials, i.e., copper, lead and tin, and also metals such as aluminium which will react with carbonaceous material, but not strongly at temperatures below the melting point of the alloy, these metals are alloyed with one or more elements and are compatible with the matrix which will react readily with the carbonaceous material to effect bonding of the carbonaceous material to the matrix by the method of the present invention.
It has been found that because of similar characteristics, carbide forming metals other than titanium, vanadium and hafnium which also appear in the fourth period of the period table of elements are suitable carbide formers, e.g., scandium calcium, manganese and iron. Although scandium carbide and Ca C are soluble in water and are not suitable for example, in bonding diamonds to grinding wheels which are to be used with water based coolants or in moist atmospheres.
A further material to which we have bonded diamond particles by a solid state process is stainless steel (i.e., an iron based alloy containing nickel and chromium).
The present invention may be used with advantage for incorporating carbon fibres in a metal matrix by dis,- tributing the carbon fibre throughout a powdered mixture of the matrix material either as a continuous tow or a chopped fibre and sintering the powdered mixture to produce a cured artefact containing the disperesed carbon fibres. The present invention greatly improves the bonding of the carbon fibres to the matrix material. By including in the powdered mixture a suitable carbide forming constituent that will react favourably with the carbon fibres to form an adherent bonding carbide layer a strong bonding carbide layer may be formed at the interface of the sintered matrix and the carbon fibre.
It is to be understood that the invention is not limited to the foregoing examples and if desired the carbide forming constituents may be implanted in the metal matrix by an ion implantation process or by a sputtering process.
We claim:
1. A solid state method of bonding a solid carbonaceous material selected from the group consisting of diamond, carbon fiber, and refractory metal carbides to a solid metal body which is principally of a metal which will not readily react with the carbonaceous material to form a carbide while the body is in the solid state comprising the steps of: incorporating in the body a metal carbide-forming constituent, said metal carbide forming constituent being dispersed within said body in a finely divided state; contacting the body with the carbonaceous material; heating the body to a temperature at which the body remains wholly solid and maintaining the body at the said temperature for a time sufficient to allow the metal carbide-forming constituent to diffuse through the body to the interface between the carbonaceous material and the body and to react in the solid state with the carbonaceous material to form a bonding carbide layer between the body and the carbonaceous material; the said metal carbide-forming constituent being one which will diffuse through the body and which will react in the solid state with the carbonaceous material to form a carbide, and the body being one which will allow the metal carbide-forming constituent to diffuse through it to the interface between the carbonaceous material and the body and to react with the carbonaceous material.
2. A method according to claim 1 wherein said solid carbonaceous material is tungsten carbide.
3. A method according to claim 1 wherein'said solid carbonaceousmaterial istitanium carbide.
body by a sputtering process.
Claims (7)
- 2. A method according to claim 1 wherein said solid carbonaceous material is tungsten carbide.
- 3. A method according to claim 1 wherein said solid carbonaceous material is titanium carbide.
- 4. A method according to claim 1 wherein said metal body is a copper-based alloy.
- 5. A method according to claim 1 wherein said metal body is an aluminum-based alloy.
- 6. A method according to claim 1 wherein said metal body is a tin-based alloy.
- 7. A method according to claim 1 wherein the metal carbide forming constituent is implanted into the metal body by an ion-implantation process.
- 8. A meThod according to claim 1 wherein the metal carbide forming constituent is implanted into the metal body by a sputtering process.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2146070 | 1970-05-04 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3778261A true US3778261A (en) | 1973-12-11 |
Family
ID=10163319
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US00139837A Expired - Lifetime US3778261A (en) | 1970-05-04 | 1971-05-03 | Manufacturing composite articles |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US3778261A (en) |
| DE (1) | DE2121969A1 (en) |
| FR (1) | FR2091202A5 (en) |
| GB (1) | GB1343427A (en) |
| IE (1) | IE35184B1 (en) |
| IT (1) | IT942412B (en) |
| NL (1) | NL7106096A (en) |
| SE (1) | SE379791B (en) |
| ZA (1) | ZA712842B (en) |
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2800700A1 (en) * | 1977-01-25 | 1978-07-27 | Lodding Engineering Corp | DEVICE FOR CREPE PRODUCTION OR FOR STRIPPING CREEPERWAYS |
| US4484644A (en) * | 1980-09-02 | 1984-11-27 | Ingersoll-Rand Company | Sintered and forged article, and method of forming same |
| US4891338A (en) * | 1987-01-13 | 1990-01-02 | Lanxide Technology Company, Lp | Production of metal carbide articles |
| US5082807A (en) * | 1987-01-13 | 1992-01-21 | Lanxide Technology Company, Lp | Production of metal carbide articles |
| US5120495A (en) * | 1990-08-27 | 1992-06-09 | The Standard Oil Company | High thermal conductivity metal matrix composite |
| US5254509A (en) * | 1987-01-13 | 1993-10-19 | Lanxide Technology Company, Lp | Production of metal carbide articles |
| EP0619378A1 (en) * | 1993-04-06 | 1994-10-12 | Sumitomo Electric Industries, Limited | Diamond reinforced composite material and method of preparing the same |
| US5401694A (en) * | 1987-01-13 | 1995-03-28 | Lanxide Technology Company, Lp | Production of metal carbide articles |
| US5677372A (en) * | 1993-04-06 | 1997-10-14 | Sumitomo Electric Industries, Ltd. | Diamond reinforced composite material |
| US20050227590A1 (en) * | 2004-04-09 | 2005-10-13 | Chien-Min Sung | Fixed abrasive tools and associated methods |
| US20070092727A1 (en) * | 2004-06-01 | 2007-04-26 | Ceratizit Austria Gesellschaft Mbh | Wear part formed of a diamond-containing composite material, and production method |
| CN117025998A (en) * | 2023-10-09 | 2023-11-10 | 赣州金顺科技有限公司 | Heat dissipation substrate embedded with diamond copper and preparation method thereof |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5253720A (en) * | 1975-10-29 | 1977-04-30 | Hitachi Ltd | Non-orientated cu-carbon fiber compoite and its manufacturing method |
| DE3367181D1 (en) * | 1982-04-06 | 1986-12-04 | Secr Defence Brit | Process for the diffusion bonding of aluminium based materials |
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| US1794300A (en) * | 1928-01-07 | 1931-02-24 | Gen Electric | Hard metal composition |
| US1939991A (en) * | 1931-12-17 | 1933-12-19 | Hard Metal Alloys Inc | Diamond cutting tool or the like and method of making the same |
| US1944758A (en) * | 1929-09-12 | 1934-01-23 | Gen Cable Corp | Method of making drawing dies |
| US2068848A (en) * | 1934-02-23 | 1937-01-26 | Howard W Dix | Method of forming diamondiferous abrasive compositions |
| US2121448A (en) * | 1936-02-14 | 1938-06-21 | Siemens Ag | Hard metal composition |
| US2133495A (en) * | 1937-02-15 | 1938-10-18 | Fay H Willey | Method of making a hard and compact metal for use in formation of tools, dies, etc. |
| US2134305A (en) * | 1936-03-27 | 1938-10-25 | American Cutting Alloys Inc | Method of manufacturing hard metal alloys |
| US3377696A (en) * | 1965-07-26 | 1968-04-16 | Gen Electric | Bonding diamond to molybdenum |
-
1970
- 1970-05-04 GB GB2146070A patent/GB1343427A/en not_active Expired
-
1971
- 1971-05-03 ZA ZA712842A patent/ZA712842B/en unknown
- 1971-05-03 IE IE547/71A patent/IE35184B1/en unknown
- 1971-05-03 US US00139837A patent/US3778261A/en not_active Expired - Lifetime
- 1971-05-03 SE SE7105716A patent/SE379791B/xx unknown
- 1971-05-03 IT IT68454/71A patent/IT942412B/en active
- 1971-05-04 NL NL7106096A patent/NL7106096A/xx unknown
- 1971-05-04 DE DE19712121969 patent/DE2121969A1/en active Pending
- 1971-05-04 FR FR7116089A patent/FR2091202A5/fr not_active Expired
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1794300A (en) * | 1928-01-07 | 1931-02-24 | Gen Electric | Hard metal composition |
| US1944758A (en) * | 1929-09-12 | 1934-01-23 | Gen Cable Corp | Method of making drawing dies |
| US1939991A (en) * | 1931-12-17 | 1933-12-19 | Hard Metal Alloys Inc | Diamond cutting tool or the like and method of making the same |
| US2068848A (en) * | 1934-02-23 | 1937-01-26 | Howard W Dix | Method of forming diamondiferous abrasive compositions |
| US2121448A (en) * | 1936-02-14 | 1938-06-21 | Siemens Ag | Hard metal composition |
| US2134305A (en) * | 1936-03-27 | 1938-10-25 | American Cutting Alloys Inc | Method of manufacturing hard metal alloys |
| US2133495A (en) * | 1937-02-15 | 1938-10-18 | Fay H Willey | Method of making a hard and compact metal for use in formation of tools, dies, etc. |
| US3377696A (en) * | 1965-07-26 | 1968-04-16 | Gen Electric | Bonding diamond to molybdenum |
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2800700A1 (en) * | 1977-01-25 | 1978-07-27 | Lodding Engineering Corp | DEVICE FOR CREPE PRODUCTION OR FOR STRIPPING CREEPERWAYS |
| US4484644A (en) * | 1980-09-02 | 1984-11-27 | Ingersoll-Rand Company | Sintered and forged article, and method of forming same |
| US5401694A (en) * | 1987-01-13 | 1995-03-28 | Lanxide Technology Company, Lp | Production of metal carbide articles |
| US4891338A (en) * | 1987-01-13 | 1990-01-02 | Lanxide Technology Company, Lp | Production of metal carbide articles |
| US5082807A (en) * | 1987-01-13 | 1992-01-21 | Lanxide Technology Company, Lp | Production of metal carbide articles |
| US5254509A (en) * | 1987-01-13 | 1993-10-19 | Lanxide Technology Company, Lp | Production of metal carbide articles |
| US5120495A (en) * | 1990-08-27 | 1992-06-09 | The Standard Oil Company | High thermal conductivity metal matrix composite |
| EP0619378A1 (en) * | 1993-04-06 | 1994-10-12 | Sumitomo Electric Industries, Limited | Diamond reinforced composite material and method of preparing the same |
| US5677372A (en) * | 1993-04-06 | 1997-10-14 | Sumitomo Electric Industries, Ltd. | Diamond reinforced composite material |
| US20050227590A1 (en) * | 2004-04-09 | 2005-10-13 | Chien-Min Sung | Fixed abrasive tools and associated methods |
| US20070092727A1 (en) * | 2004-06-01 | 2007-04-26 | Ceratizit Austria Gesellschaft Mbh | Wear part formed of a diamond-containing composite material, and production method |
| US7879129B2 (en) * | 2004-06-01 | 2011-02-01 | Ceratizit Austria Gesellschaft Mbh | Wear part formed of a diamond-containing composite material, and production method |
| CN117025998A (en) * | 2023-10-09 | 2023-11-10 | 赣州金顺科技有限公司 | Heat dissipation substrate embedded with diamond copper and preparation method thereof |
| CN117025998B (en) * | 2023-10-09 | 2024-01-16 | 赣州金顺科技有限公司 | Heat dissipation substrate embedded with diamond copper and preparation method thereof |
Also Published As
| Publication number | Publication date |
|---|---|
| IE35184L (en) | 1971-11-04 |
| ZA712842B (en) | 1972-02-23 |
| FR2091202A5 (en) | 1972-01-14 |
| IT942412B (en) | 1973-03-20 |
| DE2121969A1 (en) | 1971-11-25 |
| GB1343427A (en) | 1974-01-10 |
| NL7106096A (en) | 1971-11-08 |
| IE35184B1 (en) | 1975-12-10 |
| SE379791B (en) | 1975-10-20 |
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